NO863940D0 - OPERATED FOR AN ARTILLERY PROJECT. - Google Patents

OPERATED FOR AN ARTILLERY PROJECT.

Info

Publication number
NO863940D0
NO863940D0 NO863940A NO863940A NO863940D0 NO 863940 D0 NO863940 D0 NO 863940D0 NO 863940 A NO863940 A NO 863940A NO 863940 A NO863940 A NO 863940A NO 863940 D0 NO863940 D0 NO 863940D0
Authority
NO
Norway
Prior art keywords
ignition
propellant charge
pct
disposed
conduit
Prior art date
Application number
NO863940A
Other languages
Norwegian (no)
Other versions
NO158273B (en
NO158273C (en
NO863940L (en
Inventor
Willi Luebbers
Original Assignee
Nico Pyrotechnik
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nico Pyrotechnik filed Critical Nico Pyrotechnik
Publication of NO863940D0 publication Critical patent/NO863940D0/en
Publication of NO863940L publication Critical patent/NO863940L/en
Publication of NO158273B publication Critical patent/NO158273B/en
Publication of NO158273C publication Critical patent/NO158273C/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/40Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/16Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Air Bags (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Earth Drilling (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Golf Clubs (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
  • Sealing With Elastic Sealing Lips (AREA)
  • Braking Arrangements (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Disintegrating Or Milling (AREA)
  • Catching Or Destruction (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Vending Machines For Individual Products (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Spark Plugs (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)

Abstract

PCT No. PCT/EP86/00095 Sec. 371 Date Nov. 21, 1986 Sec. 102(e) Date Nov. 21, 1986 PCT Filed Mar. 25, 1986 PCT Pub. No. WO86/05581 PCT Pub. Date Sep. 25, 1986.A propellant charge for the reduction of base eddying or drag of a shell 12 with a centrally disposed ignition conduit and an ignition device for the charge disposed in the conduit. To improve the ignition readiness of the propellant charge, the inner surface of the propellant charge, which surrounds the ignition conduit, is formed so that it conically narrows in the aft direction. Additionally, the inner surface of the propellant charge may be provided with stepped sections. Finally, the ignition conduits disposed in the housing of the ignition device may be disposed at an angle relative to the longitudinal axis of the propellant charge so that they face the inner surface thereof.
NO863940A 1985-03-22 1986-10-03 OPERATED FOR AN ARTILLERY PROJECT. NO158273C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19853510446 DE3510446A1 (en) 1985-03-22 1985-03-22 DRIVE SET FOR SOIL REDUCTION
PCT/EP1986/000095 WO1986005581A1 (en) 1985-03-22 1986-02-25 Propulsion means for reducing the base drag

Publications (4)

Publication Number Publication Date
NO863940D0 true NO863940D0 (en) 1986-10-03
NO863940L NO863940L (en) 1986-10-03
NO158273B NO158273B (en) 1988-05-02
NO158273C NO158273C (en) 1988-08-10

Family

ID=6266060

Family Applications (1)

Application Number Title Priority Date Filing Date
NO863940A NO158273C (en) 1985-03-22 1986-10-03 OPERATED FOR AN ARTILLERY PROJECT.

Country Status (16)

Country Link
US (1) US4754704A (en)
EP (1) EP0215829B1 (en)
JP (1) JPS62501030A (en)
AT (1) ATE75031T1 (en)
AU (1) AU580860B2 (en)
CA (1) CA1271083A (en)
DE (2) DE3510446A1 (en)
DK (1) DK448486A (en)
ES (1) ES8707607A1 (en)
FI (1) FI864530A (en)
GR (1) GR860347B (en)
IL (1) IL78035A0 (en)
NO (1) NO158273C (en)
NZ (1) NZ215536A (en)
WO (1) WO1986005581A1 (en)
ZA (1) ZA861796B (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE460872B (en) * 1986-09-05 1989-11-27 Kurt Goeran Andersson THE BASE FLOOD SAGGAT FOR GRANATES AND PROJECTILES
SE461477B (en) * 1987-02-10 1990-02-19 Bofors Ab DEVICE AT A BASIC FLOW SEAT
US4920883A (en) * 1989-01-27 1990-05-01 Halliburton Logging Services, Inc. Detonation transfer methods and apparatus
US5269224A (en) * 1990-08-30 1993-12-14 Olin Corporation Caseless utilized ammunition charge module
GB9216295D0 (en) * 1992-07-31 1998-05-06 Secr Defence Long range artillery range
BE1006592A3 (en) * 1992-08-11 1994-10-25 Rion Raymond Pyrotechnic igniter for drag reduction motor
IL107763A0 (en) * 1993-11-26 1994-02-27 State Of Isreal Ministery Of D Infrared microscope
US5623115A (en) * 1995-05-30 1997-04-22 Morton International, Inc. Inflator for a vehicle airbag system and a pyrogen igniter used therein
FR2817955B1 (en) * 2000-12-13 2003-05-16 Giat Ind Sa PRIMING DEVICE FOR EXPLOSIVE CHARGE AND FORMED CHARGE INCORPORATING SUCH A PRIMING DEVICE
US6530327B2 (en) * 2001-04-23 2003-03-11 Dmd Systems, Llc Method and apparatus for burning pyrotechnic compositions
US6727485B2 (en) * 2001-05-25 2004-04-27 Omnitek Partners Llc Methods and apparatus for increasing aerodynamic performance of projectiles
US7150232B1 (en) 2001-05-25 2006-12-19 Omnitek Partners Llc Methods and apparatus for increasing aerodynamic performance of projectiles
US7802520B2 (en) * 2007-07-25 2010-09-28 Martin Electronics Drag minimizing projectile delivery system
KR101153989B1 (en) 2009-11-16 2012-06-08 한국항공대학교산학협력단 Hybrid rocket fuel with grain port of tapered shape
KR100968878B1 (en) * 2010-04-02 2011-05-31 (주)제이제이테크 Propellant disposal device for propulsion system
FR2997179B1 (en) * 2012-10-22 2015-01-16 Roxel France COMBINED DEVICE FOR DRIVING TRAJECTORY AND TRAINING REDUCTION.
US9992758B2 (en) 2013-02-15 2018-06-05 Nxp Usa, Inc. Search method and apparatus for a communication system
US10852106B2 (en) * 2014-08-22 2020-12-01 Meals, Llc Firearm ammunition with projectile housing propellant

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR715614A (en) * 1930-04-26 1931-12-07 Anciens Ets Skoda Projectiles such as flammable projectiles, mines, bombs or the like
US2613604A (en) * 1950-06-02 1952-10-14 Robert A Pyle Projectile booster
US2921521A (en) * 1958-04-25 1960-01-19 Haye Frank La Gas generator assembly
NL6604061A (en) * 1965-06-16 1966-12-19
NL135093C (en) * 1966-03-22
US3687080A (en) * 1969-03-13 1972-08-29 Messerschmitt Boelkow Blohm Gas generator and tubular solid charge construction therefore
CH511416A (en) * 1969-08-05 1971-08-15 Oerlikon Buehrle Ag Luminous bullet
US3902424A (en) * 1973-12-07 1975-09-02 Us Army Projectile
FR2328938A1 (en) * 1975-10-22 1977-05-20 Gunners Nils Eric PROJECTILE LAUNCHED BY CANNON AND PROVIDED WITH A SYSTEM REDUCING BASE TRAINANCE
FR2353040A1 (en) * 1976-05-25 1977-12-23 Europ Propulsion LIGHTER FOR PROPULSIVE POWDER BLOCK
DE2623994B2 (en) * 1976-05-26 1980-04-30 Siemens Ag, 1000 Berlin Und 8000 Muenchen Pressure or differential pressure measuring device
US4148187A (en) * 1976-11-05 1979-04-10 Hercules Incorporated Radial end burner rocket motor
CH622883A5 (en) * 1977-07-21 1981-04-30 Oerlikon Buehrle Ag
DE3151673A1 (en) * 1981-12-28 1983-07-07 Dynamit Nobel Ag, 5210 Troisdorf FLAME GUIDE FOR DRIVE CHARGE LIGHTER
DE3246380A1 (en) * 1982-12-15 1984-06-20 Diehl GmbH & Co, 8500 Nürnberg DEVICE FOR REDUCING THE FLOOR RESISTANCE OF SHOTS
DE3437250A1 (en) * 1984-10-11 1986-04-17 Rheinmetall GmbH, 4000 Düsseldorf DRIVING SET FOR SOIL REDUCTION FOR AN ARTILLERY BULLET
US4574700A (en) * 1984-11-15 1986-03-11 The United States Of America As Represented By The Secretary Of The Air Force Solid rocket motor with nozzle containing aromatic amide fibers
FR2583157B1 (en) * 1985-06-06 1987-11-20 Poudres & Explosifs Ste Nale IGNITER FOR SHELL GAS GENERATOR LOADS

Also Published As

Publication number Publication date
DK448486D0 (en) 1986-09-18
WO1986005581A1 (en) 1986-09-25
DE3684843D1 (en) 1992-05-21
FI864530A0 (en) 1986-11-07
DK448486A (en) 1986-11-03
JPH0411800B2 (en) 1992-03-02
ATE75031T1 (en) 1992-05-15
NO158273B (en) 1988-05-02
JPS62501030A (en) 1987-04-23
AU580860B2 (en) 1989-02-02
US4754704A (en) 1988-07-05
GR860347B (en) 1986-06-26
EP0215829A1 (en) 1987-04-01
ES553068A0 (en) 1987-08-16
NZ215536A (en) 1987-11-27
NO158273C (en) 1988-08-10
AU5543386A (en) 1986-10-13
ZA861796B (en) 1986-11-26
DE3510446A1 (en) 1986-09-25
ES8707607A1 (en) 1987-08-16
EP0215829B1 (en) 1992-04-15
FI864530A (en) 1986-11-07
CA1271083A (en) 1990-07-03
IL78035A0 (en) 1986-07-31
NO863940L (en) 1986-10-03

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